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model implementation for dynamic computation of system cost for advanced life supportLife support system designs for long-duration space missions have a multitude of requirements drivers, such as mission objectives, political considerations, cost, crew wellness, inherent mission attributes, as well as many other influences. Evaluation of requirements satisfaction can be difficult, particularly at an early stage of mission design. Because launch cost is a critical factor and relatively easy to quantify, it is a point of focus in early mission design. The method used to determine launch cost influences the accuracy of the estimate. This paper discusses the appropriateness of dynamic mission simulation in estimating the launch cost of a life support system. This paper also provides an abbreviated example of a dynamic simulation life support model and possible ways in which such a model might be utilized for design improvement. c2004 COSPAR. Published by Elsevier Ltd. All rights reserved.
Document ID
20050193848
Document Type
Reprint (Version printed in journal)
Authors
Levri, J. A.
(Stevens Institute of Technology Hoboken, NJ 07030, United States)
Vaccari, D. A.
Date Acquired
August 23, 2013
Publication Date
January 1, 2004
Publication Information
Publication: Advances in space research : the official journal of the Committee on Space Research (COSPAR)
Volume: 34
Issue: 7
Subject Category
Man/System Technology and Life Support
Distribution Limits
Public
Copyright
Other
Keywords
NASA Discipline Life Support Systems
Non-NASA Center